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Outgassing Effect on Spacecraft Structure Materials
Current Issue
Volume 2, 2015
Issue 4 (August)
Pages: 34-38   |   Vol. 2, No. 4, August 2015   |   Follow on         
Paper in PDF Downloads: 63   Since Sep. 3, 2015 Views: 1914   Since Sep. 3, 2015
Authors
[1]
Ahmad Anwar, National Authority for Remote Sensing and Space Science, Cairo, Egypt.
[2]
Dalia Elfiky, National Authority for Remote Sensing and Space Science, Cairo, Egypt.
[3]
Gamal Hassan, National Institute for Standards, Cairo, Egypt.
[4]
Marta Albona, Astronautics Electric and Energetic Engineering Department, Sapienza University of Rome, Rome, Italy.
[5]
Mario Marchetti, Astronautics Electric and Energetic Engineering Department, Sapienza University of Rome, Rome, Italy.
Abstract
In the vacuum deep space, outgassing has contributed to degrade mechanical performance of composite materials used in satellite. In this paper, four composite materials are used. Three types of epoxy based composite materials are tested: Carbon fiber, glass fiber and kevlar, which are used in satellite structure. The tested materials are manufactured by commercial method (hand lay-up method without autoclave curing). The forth material is polyimide which is a commercial sheet used in thermal multilayer insulator. The aim of this paper is to qualify those commercial manufacture materials to be used as Low Earth Orbit satellite structure. This study proves two important results; the use of hand lay-up Kevlar/epoxy in the satellite manufacture is rejected. While, the commercial Polyimide (Artilon®) is confirmed as a new material used in space as a layer in the multilayer insulation at the lower temperature side.
Keywords
Vacuum, Outgassing, Polymers, Glass Fiber, Carbon Fiber, Kevlar, Polyimide Composite Materials
Reference
[1]
ECSS-Q-70-52A rev.1,"Kinetic outgassing of materials for space", ECSS Secretariat ESA-ESTEC Requirements and Standards Division, 25 November 2011.
[2]
Jae-Sung Kwon, Haeyong Jung, In Seok Yeo, Tae-Ho Song, "Outgassing Characteristics of a Polycarbonate Core Material for Vacuum Insulation Panel", Vacuum, 85(2011), 839-846.
[3]
Joo-Hyun Han, Chun-Gon Kim, "Low Earth Orbit Space Environment Simulation and Its Effects on Graphite/Epoxy Composites", Composite Structures, 72(2006), 218-226.
[4]
Tribble AC., "Designing For The Space Environment", Aerospace Am 1993:26-9.
[5]
M. Hassig, K. Altwegg, H. Balsiger, "Spacecraft Outgassing, A Largely Underestimated Phenomenon", Space Sci. Rev. 128(2008), 745-801.
[6]
K. Fayazbakhsh, A. Abedian,"Materials Selection for Application in Space Environment Considering Outgassing Phenomenon", Advances in space research, 45(2010), 741-749.
[7]
Department of defense, 'composite material handbook: polymer matrix composites guidelines for characterization of structural materials', MIL-HDBK-17-1F vol. 1, Department of defense. Washington, DC; 2002.
[8]
Marta Albano, Andrea Delfni, Fabrizio Volpini, Mario Marchetti, "Outgassing Test Report", SASLab, Sapienza university of Rome, 2014.
[9]
ASTM standard E 595, 'Standard test methods for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in Vacuum Environment", 1999.
[10]
ECSS-Q-70-71A rev.1, "Space Product Assurance, Data for selection of Space Materials and Processes", ECSS Secretariat ESA-ESTEC Requirements and Standards Division, 18 June 2004.
[11]
ECSS-Q-ST-70-02C rev.1, "Thermal Vacuum Outgassing Test For The Screening Of Space Materials ",ECSS Secretariat ESA-ESTEC Requirements and Standards Division, 15 November 2008.
[12]
E. Grossman, I. Gouzman, "Space Environment Effects on Polymers in Low Earth Orbit”, Nuclear instruments and methods, B208 (2003), 48-57.
[13]
Sang Yoon Park, Heung Soap Choi, Won Jong Choi, Hyuk Kwon,"Effect of vacuum thermal cyclic exposures on unidirectional carbon fiber/epoxy composites for low earth orbit space applications", Composites: Part B, 43 (2012), 726–738.
[14]
Martin, D.J., Carl, R.M. ''The influence of commonly used materials and compounds on Spacecraft contamination". Acta Astronautica, 30(1993), 51–65.
[15]
R. Destefanis, E. Amerio, M. Briccarello, M. Belluco, M. Faraud, E. Tracino, C. Lobascio, " Space Environment Characterization Of Kevlar®: Good For Bullets, Debris And Radiation Too", 2010.
[16]
http://www.outgassing.nasa.gov/cgi/uncgi)
[17]
http://www.netcomposites.com/
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